Beech 1900C

Service difficulty reports · 1,841

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '1900C'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 99ZZZX4631Switch · out of adjustNOSE GEAR DOWN AND LOCKED LIGHTS FAILED TO ILLUMINATE WITH LANDING GEAR SELECTED DOWN FOR LANDING AT NOME, ALASKA. AN UNEVENTFUL LANDING WAS PERFORMED AT NOME. THE PILOT VISUALLY INSPECTED THE GEAR AFTER LANDING AND AFTER WIGGLING THE NOSE GEAR DOWN AND LOCKJul 22, 1999 · N5632C · Beech 1900C · Landing Gear Position and WarningSDR 20000502AP014Bulkhead · crackedDURING A ROUTINE ACE CAMP INSPECTION NR 6, HEAVY AFT FUSELAGE AND EMPENNAGE, FOUND MULTIPLE CRACKS IN CANTED BULKHEAD, STATION 588.10, IN EXCESS OF CRACK LIMITS PROVIDED IN BEECHCRAFT SERVICE BULLETIN 2564, REV 1 INCORPORATION OF SB 2564 KIT NR 129-4005-1S BEIJul 12, 1999 · N45GL · Beech 1900C · Fuselage Main, BulkheadSDR 99ZZZX3458Windshield · crackedPILOT'S WINDSHIELD CRACKED IN-FLIGHT. LANDED AT GAL. NOT E: WINDSHIELD HUMP SEALS HAD BEEN REPLACED ON 6-23-99.Jul 5, 1999 · N575Q · Beech 1900C · Flight Compartment WindowsSDR AU990426Circuit Breaker · failed(AUS) LANDING GEAR 60 AMP CIRCUIT BREAKER LOCATED IN THE LT ENGINE NACELLE TRIPPED. SUSPECT CAUSED BY WATER INGRESS.Apr 30, 1999 · Beech 1900C · Landing Gear Retraction/Extension SystemSDR AU990424Indicator · inaccurate(AUS) AIRSPEED INDICATOR HAS INCORRECT READINGS.Apr 30, 1999 · Beech 1900C · Airspeed/Mach IndicatorSDR 20000502AP015Skin · crackedON ROUTINE INSPECTION, FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT FUSELAGE STATION 544.25, WATER LINE 113.00. THIS LOCATION HAS A BULKHEAD AND STRINGER JOINT LOCATED BEHIND IT. THE BULKHEAD FLANGE WAS ALSO CRACKED AT THIS LOCATION. NO CAUSE FOR THE CRACK COUApr 18, 1999 · N41UE · Beech 1900C · Fuselage Main, Plate/SkinSDR 20000502AP016Housing · erodedON PREFLIGHT INSPECTION, NOTICED OIL LEAKING FROM NR 2 ENGINE. FOUND PIN HOLE IN ENGINE SCAVENGE PUMP HOUSING. TEAR DOWN INSPECTION REVEALED DEEP CAVITATION WEAR THAT HAD PERFORMED THE PUMP BODY WALL. THIS PUMP HOUSING WAS IN COMPLIANCE WITH PWA S/B 13088 CApr 6, 1999 · N41UE · Beech 1900C · Turbine Engine Oil SystemSDR 20000502AP017Cooler · crackedMECHANICS NOTICED OIL LEAKING FROM NR 1 ENGINE LOWER CHIN COWLING. REMOVED COWLING AND FOUND OIL COOLER LEAKING AT EDGE WELD. REPLACED OIL COOLER WITH 0 TSN UNIT. SERVICED OIL RESERVOIR WITH 2 QUARTS. THIS IS THE SECOND OIL COOLER TO FAIL ON THIS AIRCRAFTSApr 3, 1999 · N5632C · Beech 1900C · Engine Oil CoolerSDR 20000505AP027Cooler · crackedTWENTY MINUTES SOUTH OF BARROW, AK, LOST OIL PRESSURE ON NR 1 ENGINE AND LOW OIL PRESSURE LIGHT CAME ON. ENGINE SECURED AND AN UNEVENTFUL LANDING WAS EXECUTED. VERIFIED LOW OIL LEVEL. VERIFIED CRACKED OIL COOLER. REPLACED OIL COOLER AND COMPLIED WITH OIL FMar 29, 1999 · N5632C · Beech 1900C · Engine Oil CoolerSDR 20010501CW018Fuel Heater · crackedLOWER BOTTOM PLADE CRACKED AT EDGE WELD. LARGE QUANTITY OF OIL LOST. THIS IS THE SECOND FAILURE, CRACK, ON THIS FUEL HEATER IN 40.8 HOURS. SUSPECT IMPROPER/POOR REPAIR AND TEST PROCEDURES AT OVERHAUL BY VENDOR.Mar 12, 1999 · N5632C · Beech 1900C · Fuel HeaterSDR 99ZZZM237Fire Light · illuminatedFLT 9376 - MIA-FLL - LEFT FIREWALL FUEL VALVE ILLUMINATED ON TAXIWAY IN MIA. NO SMOKE OR FLAMES OBSERVED BUT HANDLE STAYED LIT UNITL BATTERY TURNED OFF. INSPECTED LEFT ENGINE FIRE LOOP FOR CHAFING OR LOOSE CONNECTIONS. NO DEFECTS NOTED. GROUND RUN LEFT ENGMar 10, 1999 · N86UE · Beech 1900C · Fire DetectionSDR 99ZZZM235Sensor · failedFLT 9149 - FPO-FLL, LANDING GEAR WILL NOT EXTEND HAD TO MANUALLY EXTEND GEAR. REPLACED HYDRAULIC LOW LEVEL SWITCH. PERFORMED LANDING GEAR EXTENSION/RETRACTION CHECK. OPS CHECK NORMAL. (M)Mar 8, 1999 · N190GA · Beech 1900C · Landing Gear Retraction/Extension SystemSDR 99ZZZM238Circuit Breaker · trippedFLT 9233 - FLL-EYW - LANDING GEAR WOULD NTO GO DOWN. HAD TO PUMP DOWN. INSPECTED SYSTEM. FOUND 60 AMP CIRCUIT BREAKER IN LEFT NACELLE TO BE TRIPPED. RESET CIRCUIT BREAKER. PERFORMED SEVERAL SATISFACTORY RETRACTION CHECKS. (M)Mar 5, 1999 · N105GL · Beech 1900C · Landing Gear Retraction/Extension SystemSDR 99ZZZX1147Fuel Pump · failed67.6 HOURS AFTER OVERHAUL, DRIVESHAFT BROKE. PUMP TURNS NORMAL, NO DAMAGE DETECTED INSIDE PUMP.Mar 2, 1999 · N45GL · Beech 1900C · Engine Fuel PumpSDR 99ZZZM236Power Pack · failedFLT 9332 - EYW-TPA - LANDING GEAR CIRCUIT BREAKER POPPED IN FLIGHT. RESET AND POPPED AGAIN. EXTENDED GEAR VIA ALTERNATE GEAR EXTENSION PROCEDURES. REPLACED POWER PACK MOTOR. PERFORMED SATISFACTORY LANDING GEAR RETRACTION/EXTENSION CHECKS. (M)Feb 19, 1999 · N199GA · Beech 1900C · Landing Gear Retraction/Extension SystemSDR 99ZZZX1957Pe Line · brokenKTN/FAI - EN ROUTE, RIGHT ENGINE TORQUE WENT TO ZERO. N1 STABLE AT IDLE. FUEL FLOW NORMAL FOR IDLE. POWER LEVER AND CONDITION LEVER HAD NO EFFECT. DIVERTED TO JUNEAU. REPLACED P1 LINE.Feb 14, 1999 · N575P · Beech 1900C · Fuel Controlling SystemSDR 99ZZZM183Switch Cam · looseAFTER DEPARTURE, GEAR SELECTED UP AND NOSE GEAR RETRACTED BUT MAINS DID NOT. GEAR SELECTED DOWN AND GEAR SHOWED DOWN AND LOCKED. GEAR SELECTED UP AGAIN AND GEAR WOULD NOT RETRACT. GEAR SELECTED DOWN AND INDICATED THREE GREEN. AIRCRAFT RETURNED TO AIRPORT AJan 27, 1999 · N1563C · Beech 1900C · Landing Gear Position and WarningSDR 99ZZZM184Line · rupturedPILOT REPORTED CAPTAINS LEFT BRAKE VERY WEAK. BRAKE SYSTEM BLEED, OPS CHECKED GOOD. THE NEXT DAY, THE FLEXIBLE BRAKE LINES (UPPER) IN THE GEAR WELLS, LEFT AND RIGHT, WERE FOUND TO BE LEAKING THROUGH THE HOSE. REPLACED UPPER FLEX LINE. (M)Jan 25, 1999 · N45GL · Beech 1900C · Landing Gear Brake SystemSDR CA990119045Generator · contaminated(CAN) GENERATOR U/S. NO START FUNCTION AFTER LANDING. COMMUTATOR CONTAMINATED WITH OIL AND HAD SHORTED.Dec 28, 1998 · Beech 1900C · Starter-GeneratorSDR CA990129004Bearing · corroded(CAN) CORROSION - SEAL AREA BEARING.Dec 23, 1998 · Beech 1900C · Propeller AssemblySDR 99ZZZM186Oil Cooler · crackedAFTER DEPARTURE FROM FAI, PILOT NOTICED LOW OIL PRESSURE LIGHT ON LEFT ENGINE FLICKER, OBSERVED OIL PRESSUR GAUGE DROPPING SLOWLY AND PERFORMED A PRECAUTIONARY SHUT DOWN ON THAT ENGINE. OIL PRESSURE WAS AT 65 PSI AT THE TIME OF SHUTDOWN. AIRCRAFT RETURNED FORDec 22, 1998 · N1563C · Beech 1900C · Engine Oil CoolerSDR CA990111059Generator · overheated(CAN) GENERATOR LIGHT ON IN-FLIGHT. NO STARTER FUNCTION AFTER LANDING. BURNT ELECTRICAL SMELL AT GENERATOR. REPLACED GENERATOR.Dec 16, 1998 · Beech 1900C · Starter-GeneratorSDR 99ZZZM185Heater · crackedAPPROX ONE HOUR INTO THE FLIGHT, THE RIGHT LOW ENGINE OIL PRESSURE LIGHT FLICKERED. THE PILOT CHECKED THE OIL PRESSURE GAUGE AND FOUND IT DOWN TO ABOUT 60 PSI. POWER WAS REDUCED AND THE AIRCRAFT WAS DIVERTED TO A CLOSE AIRPORT WHERE AN UNEVENTFUL SAFE LANDINDec 9, 1998 · N31240 · Beech 1900C · Fuel HeaterSDR NSVA9810281Latch · failedRIGHT SIDE COWLING CAME LOOSE IN FLIGHT. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. COWLING REMAINED ATTACHED TO THE NACELLE. MAINTENANCE VISUALLY INSPECTED RT COWLING AND FOUND INBOARD COWLING LATCH FAILED. MAINTENANCE REMOVED AND REPLACED THE COWLING LATCH Oct 27, 1998 · N550CJ · Beech 1900C · Engine Cowling SystemSDR 98ZZZX4682Line · leakingTHIS FUEL LINE GOES FROM THE FCU TO THE FUEL FLOW TRANSMITTER. THE DUCT FROM THE COWL TO THE STARTER/GENERATOR RUBS ON THIS LINE. THIS IS ONLY ON THE LEFT ENGINE. THIS DUCT RUBBED A HOLE IN THIS HIGH PRESSURE FUEL LINE. SUBMITTER STATED THEY HAVE CHANGED 2Oct 17, 1998 · N207CJ · Beech 1900C · Aircraft Fuel Distribution SystemSDR 98ZZZX4217Fuel Cell · contaminatedTHE WING IS CONSTRUCTED IN A WAY THAT TRAPPED WATER CANNOT BE DRAINED FROM THE TRAILING EDGE OF THE FUEL STORAGE AREA BETWEEN WS 171.29 AND WS 183.07. THE SAME PROBLEM IS IN BOTH WINGS. A DRAIN PATH NEEDS TO BE PROVIDED.Oct 16, 1998 · N5632C · Beech 1900C · Fuel StorageSDR 98ZZZM904Power Pack · inoperativePILOT REPORTE THE LANDING GEAR SYATED DOWN WHEN SELECTED UP AND THE LANDING GEAR RELAY CIRCUIT BREAKER POPPED. THE LANDING GEAR CONTINUED TO SHOW THREE GREEN DOWN AND LOCKED LIGHTS. A NORMAL LANDING WAS PERFORMED. MAINTENANCE DETERMINED THE HYDRAULIC POWER Oct 10, 1998 · N31240 · Beech 1900C · Landing Gear Retraction/Extension SystemSDR CA981014016Switch · malfunctioned(CAN) DURING A NORMAL BUSHING CHANGE ON THE MAIN LANDING GEAR TORQUE LINK, THE LANDING GEAR SAFETY SWITCH WAS REMOVED. ON REINSTALLATION AND RIGGING, THE LANDING GEAR WAS NOT COMPLETELY COMPRESSED AND LANDING GEAR WOULD NOT RETRACT. THEREFORE, RIGGING OF THE Oct 1, 1998 · Beech 1900C · Main Landing Gear Strut/Axle/TruckSDR 98ZZZX3820Indicator · malfunctionedMIA/TPA - FLT 9325 - PILOT REPORT: GEAR HANDLE 'RED' INTRANSIT LIGHTS ILLUMINATED IN-FLIGHT. INSPECTED GEAR WARNING SYSTEM, PERFORMED GEAR EXTENSION AND RETRACTION OPERATIONAL CHECKS ON JACKS. COULD NOT DUPLICATE DISCREPANCY.Sep 27, 1998 · N86UE · Beech 1900C · Landing Gear Position and WarningSDR 98ZZZX3822Cable · brokenMIA/MCO - FLT 9380 - FORWARD CABIN DOOR WILL NOT OPEN WHEN HANDLE IS ROTATED. REMOVED AND REPLACED BROKEN DOOR CABLE.Sep 22, 1998 · N198GA · Beech 1900C · Passenger/Crew DoorsSDR 98ZZZX3824Indicator · malfunctionedMCO/EYW - FORWARD CABIN DOOR ANNUNCIATOR ILLUMINATED IN-FLIGHT. CAPTAIN PERFORMED EMERGENCY DIVERSION INTO RSW. SUBMITTER STATED DETERMINED TO BE AN INDICATION PROBLEM, DEFERRED.Sep 21, 1998 · N138GL · Beech 1900C · Door Warning SystemSDR 98ZZZX3821Indicator · malfunctionedRSW/TPQ - FLT 9136 - LANDING GEAR HANDLE ILLUMINATED IN-FLIGHT. GEAR HORN ALSO SOUNDED. GEAR HANDLE WAS IN UP POSITION, COULD NOT SILENCE HORN. PERFORMED LANDING GEAR RETRACTION, CHECKED ALL WIRES, SWITCHES, AND PC BOARDS. COULD NOT DUPLICATE.Sep 20, 1998 · N11ZR · Beech 1900C · Landing Gear Position and WarningSDR CA981125078Motor · separated(CAN) AFTER LANDING, FLAPS SELECTED FROM 17 DEGREES TO ZERO DEGREES. THE FLAPS DID NOT RESPOND. MAINTENANCE FOUND THAT THE TRANSMISSION/MOTOR ASSEMBLY HAD INTERNALLY SEPARATED AND THE ASYMMETRY SWITCH LOCKED OUT FURTHER MOVEMENT. THE TRANSMISSION/MOTOR WAS Sep 18, 1998 · Beech 1900C · Trailing Edge Flap Control SystemSDR 98ZZZX4118Spar · corrodedFOUND MAIN SPAR LOWER CAP SEVERELY CORRODED. THIS CORROSION WAS FOUND WHERE MAIN SPAR PASSES THROUGH FUSELAGE BENEATH AIR CONDITIONER LOCATION. SUSPECT MOISTURE FROM AIR CONDITIONER COLLECTED ON SPAR CAUSING CORROSION. LOCATION FURTHER IDENTIFIED AS FS 288.Sep 16, 1998 · N5632C · Beech 1900C · Wing SparSDR 98ZZZX3823Duct · leakingTPA/FLL - FLT 9175 - WHEN RIGHT BLEED AIR IS PLACED IN ON POSITION, RUBBER BURNING SMELL IS DETECTED THROUGHOUT CABIN. REMOVED EXCESSIVE AMOUNTS OF SEALANT FROM RIGHT BLEED AIR PLUMBING. TEST FLIGHT ACCOMPLISHED SATISFACTORY.Sep 11, 1998 · N126UE · Beech 1900C · Engine Bleed Air SystemSDR CA980922024Bearing · stiff(CAN) CREW REPORTED STEERING AS BEING STIFF ACCOMPANIED WITH A GRINDING NOISE. UPON INVESTIGATION, THE LOWER RUDDER BEARING WAS FOUND TO BE STIFF TO MOVE. THE CENTER ATTACHMENT BOLT WAS SEIZED TO THE BEARING AND HAD TO BE DRILLED OFF THE BELLCRANK. NEW BEARISep 2, 1998 · Beech 1900C · Rudder/Tab, Attach FittingsSDR 98ZZZM832Spar · corrodedFOUND CORROSION ON FORWARD SIDE OF MAIN WING SPAR LOWER CAP BOND ASSY. THE AFFECTED AREA IS UNDER THE CABIN FLOOR IN THE CABIN. CORROSION WAS FOUND ON THE FORWARD FACE OF THE SPAR CAP AND WAS DISTRIBUTED IN SMALL AREAS ACROSS THE SPAR, JUST ABOVE THE EDGE OFAug 29, 1998 · N1563C · Beech 1900C · Wing SparSDR 98ZZZX3399Relay · contaminatedLANDING GEAR FAILED TO EXTEND WITH GEAR HANDLE SELECTION. LANDING GEAR EXTENDED USING HAND PUMP SYSTEM, GEAR INDICATIONS WERE NORMAL. FOUND LANDING GEAR PUMP RELAY CONTAMINATED WITH WATER AND SUSPECT UNIT FROZE IN-FLIGHT AND FAILED TO POWER ELECTRIC PUMP. SAug 27, 1998 · N45GL · Beech 1900C · Landing Gear Retraction/Extension SystemSDR 98ZZZX3398Spar · corrodedFOUND CORROSION ON FORWARD SIDE OF MAIN WING SPAR LOWER CAP BOND ASSY. THE AFFECTED AREA IS UNDER THE CABIN FLOOR IN THE CABIN. CORROSION WAS FOUND ON THE FORWARD FACE OF THE SPAR AND WAS DISTRIBUTED IN SMALL AREAS ACROSS THE SPAR JUST ABOVE THE EDGE OF THE Aug 23, 1998 · N41UE · Beech 1900C · Wing SparSDR 98ZZZX3397Spar Cap Assy · corrodedFOUND CORROSION ON FORWARD SIDE OF MAIN WING SPAR LOWER CAP BOND ASSY. THE AFFECTED AREA IS UNDER THE CABIN FLOOR IN THE CABIN. CORROSION WAS FOUND ON THE FORWARD FACE OF THE SPAR AND WAS DISTRIBUTED IN SMALL AREAS ACROSS SPAR JUST ABOVE THE EDGE OF THE SEALAug 20, 1998 · N45GL · Beech 1900C · Wing SparSDR CA980827014Bleed Air Line · cracked(CAN) THE BLEED AIR LINE BLEW OUT A TRIANGULAR PIECE OF MATERIAL APPROXIMATELY .25 INCH IN SIZE AT THE OUTSIDE OF THE BEND RADIUS JUST BEYOND THE THRESHOLD OF THE NACELLE. ABRASION MARKS WERE VISIBLE DIRECTLY OVER THE CRACKED AREA AND BLOWN BACK AREA. THIS CAug 14, 1998 · Beech 1900C · Pneumatic Distribution SystemSDR AU981140Blade · damaged(AUS) LEFT ENGINE FIRST STAGE COMPRESSOR BLADES (8 OFF) SUFFERED REPAIRABLE FOD DAMAGE. THE FOD WAS THEN DEFLECTED BACK THROUGH THE INLET SCREEN.Aug 12, 1998 · Beech 1900C · Turbine Engine Compressor SectionSDR CA980818031Windshield · cracked(CAN) DURING FLIGHT, A LOUD NOISE WAS HEARD. A VISUAL CHECK REVEALED COPILOT'S WINDOW HAD CRACKED. AIRCRAFT RETURNED TO DEPARTURE BASE. MAINTENANCE CHECK REVEALED ONLY OUTER PLY OF WINDOW HAD CRACKED. AIRCRAFT FERRIED BACK TO MAINTENANCE BASE PER MEL AND WIAug 11, 1998 · Beech 1900C · Flight Compartment WindowsSDR 20010426CW001Spar Cap · corrodedFOUND CORROSION ON FORWARD SIDE OF MAIN WING SPAR LOWER CAP BOND ASSEMBLY. THE AFFECTED AREA IS UNDER THE CABIN FLOOR IN THE CABIN. CORROSION DAMAGE FOUND TO REQUIRE REPLACEMENT OF THE SPAR CAP BOND ASSEMBLY.Aug 9, 1998 · N5632C · Beech 1900C · Wing, Center BoxSDR CA980819012Bleed Air Line · leaking(CAN) RIGHT HAND BLEED AIR LIGHT AND MASTER CAUTION LIGHTS ILLUMINATED SHORTLY AFTER TAKEOFF. AIRCRAFT SAFELY RETURNED TO DEPARTURE BASE. MAINTENANCE CHECK FOUND A BLEED AIR LINE HAD DEVELOPED A SMALL PIN HOLE WHICH ALLOWED AIR TO ESCAPE REDUCING PRESSURE INAug 5, 1998 · Beech 1900C · Pneumatic Distribution SystemSDR 98ZZZM614Switch · looseFLT 2020 - FLL-MIA - GEAR UNSAFE LIGHT ILLUMINATED AND RIGHT GEAR DOWN AND LOCKED ANNUNCIATOR EXTINGUISHES ON GROUND WHEN RIGHT BRAKE IS DEPRESSED. SECURED RIGHT MAIN GEAR DOWNLOCK SWITCH. (M)Jul 31, 1998 · N155GA · Beech 1900C · Landing Gear Position and WarningSDR 98ZZZX2873Actuator · failedFPO/FLL - FLT 9149 - NOSE GEAR INDICATOR FAILED TO ILLUMINATE WITH GEAR EXTENDED. AIRCRAFT LANDED SAFELY AND WAS FERRIED TO MIAMI. REMOVED AND REPLACED NOSE GEAR ACTUATOR. (X)Jul 20, 1998 · N154GA · Beech 1900C · Landing Gear ActuatorSDR 98ZZZX2872Line · crackedTCB/MIA - FLT 9138 - GEAR WARNING INOPERABLE. REMOVED AND REPLACED MANUAL BLEED VALVE LINE AT LANDING GEAR POWER PACK. (X)Jul 19, 1998 · N197GA · Beech 1900C · Landing Gear Position and WarningSDR 98ZZZX2864Switch · out of adjustPBI/MIA - FLT 9319 - NOSE GEAR LIGHT ILLUMINATED APPROXIMATELY 1-1/2 MINUTES AFTER MAIN GEAR WITH GEAR SELECTED DOWN. AIRCRAFT LANDED SAFELY. ADJUSTED NOSE GEAR MICROSWITCH.Jul 19, 1998 · N154GA · Beech 1900C · Landing Gear Position and WarningSDR 98ZZZX2874Annunciator · malfunctionedTPA/TLH - FLT 9197 - NOSE GEAR LIGHT WOULD NOT ILLUMINATE WITH GEAR SELECTED DOWN. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED GEAR DOWN AND LOCKED ANNUNCIATOR. (X)Jul 16, 1998 · N154GA · Beech 1900C · Landing Gear Position and Warning
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